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时间:2011-04-09 10:26来源:蓝天飞行翻译 作者:航空
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P514 PANEL P614 PANEL  SEE  C 
SHT 2 
P414 PANEL 
SEE  B 
MAIN EQUIPMENT CENTER 
CAPTAINS' INSTRUMENT
BUS VOLTAGE SENSE 
UNIT, M7507 
F/O INSTRUMENT  28-VOLT AC MAIN 
BUS VOLTAGE  TRANSFORMER, T94 
SENSE UNIT, M7508 
28-VOLT AC GROUND SERVICE 
BUS TRANSFORMER, T150 

P6 PANEL
A

P414 PANEL B
AC Electrical Load Distribution - Component Location Figure 102 (Sheet 1)
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
FAULT ISOLATION/MAINT MANUAL

GALLEY POWER 1  GROUND HANDLING 
ELCU, M481  UTILITY POWER 1  RELAY 1, R117 
ELCU, M3250  GROUND HANDLING 
RELAY 2, R118 
GROUND SERVICE 
SELECT RELAY, R14 
GROUND SERVICE BUS 
P514  UTILITY SELECT 
RELAY, R1168 
GROUND SERVICE BUS 
UTILITY TRANSFER 
RELAY, R1169 
P614 
GROUND SERVICE 
TRANSFER RELAY, R15 

GALLEY POWER 2 ELCU, M482
UTILITY POWER 2 SEE J ELCU, M3251
P514 AND P614 PANELS
C
P714 PANEL
D
UTILITY POWER 3 ELCU, M3252 GALLEY POWER 3 ELCU, M485
P515 MAIN DECK CARGO HANDLING BUS RELAY 2 (R992)
MAIN DECK CARGO HANDLING BUS RELAY 1 (R991)
UTILITY POWER 4 ELCU, M3253
GALLEY POWERP615
4 ELCU, M486
P515 AND P615 PANELS
E P715 AUX/EXT NO. 2 POWER CENTER
F
AC Electrical Load Distribution - Component Location (Details from Sht 1) Figure 102 (Sheet 2)
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 AC ELECTRICAL LOAD DISTRIBUTION - ADJUSTMENT/TEST
_________________________________________________
 1.  General_______
 A.  This procedure has one task to do an operational test of the ac electrical-load-distribution system. The operational test includes a test of the utility power ELCUs and the galley power ELCUs.
 TASK 24-50-00-715-001
 2.  Operational Test - AC Electrical Load Distribution (Fig. 501)__________________________________________________
 A.  References
 (1)  
24-22-00/201, Manual Control

 (2)  
WDM 24-51-11 thru 24-51-73, 24-53-21 thru 24-53-62

 (3)  
SSM 24-51-01 thru 24-51-08, 24-53-01 thru 24-53-02

 B.  
Access

 (1)  
Location Zone
 221 Control Cabin, LH


 C.  
Procedure


 S 865-002
 (1)  
Supply electrical power (Ref 24-22-00/201).

 S 715-010

 (2)
Do a test of the indicator lights for the electrical system:

 (a)  
Set the IND LTS switch, on the P5 panel, to TEST.

 (b)  
Make sure all the indicator lights for the electrical system on the P5 panel and the P461 panel come on.

 (c)  
Set the IND LTS switch to BRT.


 S 865-006
 (3)  
Make sure the BUS TIE 1, 2, 3, and 4 switches, on the P5 panel, are set to AUTO.

 (a)  
Make sure the ISLN lights on the BUS TIE switches are off.


 S 865-007
 (4)  
Make sure the OFF lights on the UTILITY switches, on the P5 panel, are off.

 (a)  
If the OFF light(s) are on, push the applicable UTILITY switch.


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 ALL  ú ú 01 Page 501 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
 
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本文链接地址:747-400 AMM 飞机维护手册 ELECTRICAL POWER 电源 2(102)